Hit-to-kill accurate minimum time continuous second-order sliding mode guidance for worst-case target maneuvers

Author:

Pushpangathan Jinraj V1,Kandath Harikumar2ORCID,Balakrishnan Ajithkumar3

Affiliation:

1. Department of Aerospace Engineering, Indian Institute of Science, Bangalore, India

2. Robotics Research Center, International Institute of Information Technology, Hyderabad, India

3. Department of Electrical Engineering, College of Engineering Trivandrum, India

Abstract

The recent research is focused on the development of an advanced interceptor missile that has hit-to-kill accuracy against ballistic targets performing evasive maneuvers. In this paper, a guidance law that achieves hit-to-kill accuracy against ballistic target executing worst-case maneuvers is developed using second-order sliding mode control and optimal control. The guidance law thus developed is continuous and has minimum time convergence for worst-case target maneuvers. The performance of the continuous guidance law with minimum time convergence is evaluated through numerical simulations against ballistic targets executing step maneuvers with changing polarity and weaving maneuvers.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Spacecraft Attitude Control with Fully Actuated System and Particle Swarm Optimization Approaches;2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA);2023-07-14

2. Adaptive second order sliding mode guidance law for missile-target interception with fuzzy logic system;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2023-04-07

3. Ballistic Missile Midcourse Intelligent Maneuver Strategy Based on PPO Algorithm;Lecture Notes in Electrical Engineering;2023

4. Sliding mode control based impact angle constrained guidance with predefined convergence time;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-10-01

5. Sliding mode–based simultaneous control of impact angle and impact time;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-07-05

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